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公开(公告)号：US20130232883A1
公开(公告)日：2013-09-12
申请号：US13875548
申请日：2013-05-02
Applicant: THE BOEING COMPANY
Inventor： Richard B. Tanner , Brian H. Korenaga , Jeffrey F. Stulc , Ian C. Burford
CPC classification number: B64C1/1461 , B64C1/1446 , E04C2/54 , E05D15/00
Abstract: A method of installing a door in an access opening in a skin of an aircraft. A composite inner door panel is positioned against an inside face of the skin. A composite outer door panel is positioned against an outside face of the skin. A plurality of fasteners is installed through fastener openings in the composite outer door panel. The plurality of fasteners is tightened to form a chamfered interface between the skin and the composite outer door panel.
Abstract translation: 一种将门安装在飞行器皮肤的进入口中的方法。 复合内门板抵靠皮肤的内表面定位。 复合外门板抵靠皮肤的外表面定位。 多个紧固件通过复合外门板中的紧固件开口安装。 多个紧固件被紧固以在皮肤和复合外门面板之间形成倒角接口。
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公开(公告)号：US09073618B2
公开(公告)日：2015-07-07
申请号：US13875548
申请日：2013-05-02
Applicant: The Boeing Company
Inventor： Richard B. Tanner , Brian H. Korenaga , Jeffrey F. Stulc , Ian C. Burford
CPC classification number: B64C1/1461 , B64C1/1446 , E04C2/54 , E05D15/00
Abstract: A method of installing a door in an access opening in a skin of an aircraft. A composite inner door panel is positioned against an inside face of the skin. A composite outer door panel is positioned against an outside face of the skin. A plurality of fasteners is installed through fastener openings in the composite outer door panel. The plurality of fasteners is tightened to form a chamfered interface between the skin and the composite outer door panel.
Abstract translation: 一种将门安装在飞行器皮肤的进入口中的方法。 复合内门板抵靠皮肤的内表面定位。 复合外门板抵靠皮肤的外表面定位。 多个紧固件通过复合外门板中的紧固件开口安装。 多个紧固件被紧固以在皮肤和复合外门面板之间形成倒角接口。
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公开(公告)号：US10793251B2
公开(公告)日：2020-10-06
申请号：US15928872
申请日：2018-03-22
Applicant: The Boeing Company
Inventor： Eric S. Kamila , Warren H. Steyaert , David D. Boes , Daniel E. McGinty , Ryan A. Fear , Renato Felicio , Eric G. Gruner , Matthew S. Elenbaas , Ian C. Burford , Eric D. Blohm
IPC: B64C3/56
Abstract: Hinge pins for foldable aircraft wings are described. An example apparatus includes a hinge pin to rotatably couple a foldable tip of an aircraft wing to a fixed structure of the aircraft wing. The hinge pin includes a first flange, a second flange spaced apart from the first flange along a central axis of the hinge pin, and a through hole oriented along the central axis.
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公开(公告)号：US20190291847A1
公开(公告)日：2019-09-26
申请号：US15928872
申请日：2018-03-22
Applicant: The Boeing Company
Inventor： Eric S. Kamila , Warren H. Steyaert , David D. Boes , Daniel E. McGinty , Ryan A. Fear , Renato Felicio , Eric G. Gruner , Matthew S. Elenbaas , Ian C. Burford , Eric D. Blohm
IPC: B64C3/56
Abstract: Hinge pins for foldable aircraft wings are described. An example apparatus includes a hinge pin to rotatably couple a foldable tip of an aircraft wing to a fixed structure of the aircraft wing. The hinge pin includes a first flange, a second flange spaced apart from the first flange along a central axis of the hinge pin, and a through hole oriented along the central axis.
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